CN215514154U - Unmanned aerial vehicle flight buffer stop - Google Patents
Unmanned aerial vehicle flight buffer stop Download PDFInfo
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- CN215514154U CN215514154U CN202121782847.1U CN202121782847U CN215514154U CN 215514154 U CN215514154 U CN 215514154U CN 202121782847 U CN202121782847 U CN 202121782847U CN 215514154 U CN215514154 U CN 215514154U
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- unmanned aerial
- aerial vehicle
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Abstract
The utility model discloses an unmanned aerial vehicle flight anti-collision device, which comprises an unmanned aerial vehicle body and connecting blocks, wherein the connecting blocks are arranged on two sides of the unmanned aerial vehicle body, one end of each connecting block is fixedly connected with a connector, one side of each connector is fixedly connected with a side surface protection device, threaded holes are formed in the connecting blocks and the connectors, mounting bolts are connected with the internal threads of the threaded holes, and a top protection device is fixedly connected to the upper surface of the unmanned aerial vehicle body. According to the utility model, through the arrangement of the side protection device, the top protection device and the front protection device, when the unmanned aerial vehicle body is collided in the flying process, the side protection device, the top protection device and the front protection device can provide a buffer protection effect for each surface of the unmanned aerial vehicle body, so that the anti-collision capability of the unmanned aerial vehicle body is greatly improved, and the damage of parts inside and outside the unmanned aerial vehicle body caused by collision is avoided.
Description
Technical Field
The utility model relates to the technical field of anti-collision devices, in particular to an unmanned aerial vehicle flight anti-collision device.
Background
The unmanned plane is called unmanned plane for short, and is an unmanned aerial vehicle operated by radio remote control equipment and a self-contained program control device. Unmanned aerial vehicles are in fact a general term for unmanned aerial vehicles, and can be defined from a technical perspective as follows: unmanned fixed wing aircraft, unmanned VTOL aircraft, unmanned airship, unmanned helicopter, unmanned multi-rotor aircraft, unmanned paravane, etc.
The anticollision ability of most unmanned aerial vehicles that have now is relatively poor, and spare part is impaired easily when the flight process bumps and makes unmanned aerial vehicle's life receive serious influence, and protector is inconvenient to be installed and is changed simultaneously.
SUMMERY OF THE UTILITY MODEL
The utility model aims to provide an unmanned aerial vehicle flight anti-collision device to solve the problems in the background technology.
In order to achieve the purpose, the utility model provides the following technical scheme: the utility model provides an unmanned aerial vehicle flight buffer stop, includes unmanned aerial vehicle body and connecting block, the both sides of unmanned aerial vehicle body all are provided with the connecting block, the one end fixedly connected with connector of connecting block, one side fixedly connected with side protector of connector, the inside screw hole that all sets up of connecting block and connector, the inside threaded connection of screw hole has the construction bolt, the last fixed surface of unmanned aerial vehicle body is connected with top protector, the positive fixedly connected with front protector of unmanned aerial vehicle body, the lower surface of unmanned aerial vehicle body is provided with the support frame.
Preferably, the side protection device comprises a first side rod, a first spring, a second side rod and an arc-shaped plate, the first spring is arranged inside the first side rod, the second side rod is fixedly connected to one end of the first spring, and the arc-shaped plate is fixedly connected to the top end of the second side rod.
Preferably, the top protector includes first mounting panel, bracing piece, second spring and roof, the last fixed surface of first mounting panel is connected with the bracing piece, the inside of first bracing piece is provided with the second spring, the top fixedly connected with roof of second spring.
Preferably, the front protection device comprises a second mounting plate, a connecting rod, a third spring and a baffle plate, wherein the connecting rod is fixedly connected to one side of the second mounting plate, the third spring is arranged inside the connecting rod, and the baffle plate is fixedly connected to one end of the third spring.
Preferably, the support frame includes support body and sucking disc, the lower surface of support body is provided with the sucking disc.
Preferably, the upper surface of the connecting block is provided with a rotating mechanism, and the upper end of the rotating mechanism is provided with a blade.
Compared with the prior art, the utility model has the beneficial effects that:
1. according to the utility model, through the arrangement of the side protection device, the top protection device and the front protection device, when the unmanned aerial vehicle body is collided in the flying process, the side protection device, the top protection device and the front protection device can provide a buffer protection effect for each surface of the unmanned aerial vehicle body, so that the anti-collision capability of the unmanned aerial vehicle body is greatly improved, and the collision is avoided to damage parts inside and outside the unmanned aerial vehicle body, thereby prolonging the service life of the unmanned aerial vehicle body.
2. According to the utility model, through the arrangement of the connector, the threaded hole and the bolt, the connecting block is aligned with the threaded hole formed in the connector during installation, and then the bolt is inserted into the threaded hole and screwed down, so that the installation can be completed, the structure is convenient to install and disassemble, and the replacement is more convenient when the protection device is damaged.
Drawings
FIG. 1 is a schematic view of the overall structure of the present invention;
FIG. 2 is a schematic view, partially in section, of a front view of the present invention;
FIG. 3 is a schematic partial cross-sectional view of a top view of the present invention;
fig. 4 is an enlarged view of the structure at a in fig. 2 according to the present invention.
In the figure: 1. an unmanned aerial vehicle body; 2. connecting blocks; 3. a connector; 4. a side guard; 401. a first side bar; 402. a first spring; 403. a second side bar; 404. an arc-shaped plate; 5. a threaded hole; 6. a bolt; 7. a top guard; 701. a first mounting plate; 702. a support bar; 703. a second spring; 704. a top plate; 8. a front face guard; 801. a second mounting plate; 802. a connecting rod; 803. a third spring; 804. a baffle plate; 9. a support frame; 901. a frame body; 902. a suction cup; 10. a rotation mechanism; 11. a blade.
Detailed Description
The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all of the embodiments. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present invention.
In the description of the present invention, it should be noted that the terms "upper", "lower", "inner", "outer", "front", "rear", "both ends", "one end", "the other end", and the like indicate orientations or positional relationships based on those shown in the drawings, and are only for convenience of description and simplicity of description, but do not indicate or imply that the referred device or element must have a specific orientation, be constructed in a specific orientation, and be operated, and thus, should not be construed as limiting the present invention. Furthermore, the terms "first" and "second" are used for descriptive purposes only and are not to be construed as indicating or implying relative importance.
In the description of the present invention, it is to be noted that, unless otherwise explicitly specified or limited, the terms "mounted," "disposed," "connected," and the like are to be construed broadly, such as "connected," which may be fixedly connected, detachably connected, or integrally connected; can be mechanically or electrically connected; they may be connected directly or indirectly through intervening media, or they may be interconnected between two elements. The specific meanings of the above terms in the present invention can be understood in specific cases to those skilled in the art.
Referring to fig. 1-4, an embodiment of the present invention is shown: the utility model provides an unmanned aerial vehicle flight buffer stop, including unmanned aerial vehicle body 1 and connecting block 2, the both sides of unmanned aerial vehicle body 1 all are provided with connecting block 2, the one end fixedly connected with connector 3 of connecting block 2, one side fixedly connected with side protector 4 of connector 3, threaded hole 5 has all been seted up to the inside of connecting block 2 and connector 3, threaded hole 5's inside threaded connection has construction bolt 6, through connector 3, threaded hole 5 and bolt 6's setting, the screw hole 5 of seting up earlier with the inside of connecting block 2 and connector 3 aligns during the installation, it can accomplish the installation to insert screw hole 5 with bolt 6 again, the structure is convenient for install and dismantle, it is more convenient to change when protector damages, the last fixed surface is connected with top protector 7 of unmanned aerial vehicle body 1, unmanned aerial vehicle body 1's positive fixedly connected with front protector 8, through side protector 4, Top protector 7 and front protector 8's setting, when unmanned aerial vehicle body 1 receives the collision at the flight process, side protector 4, top protector 7 and front protector 8 can provide a buffer protection's effect to each face of unmanned aerial vehicle body 1, very big promotion unmanned aerial vehicle body 1's anticollision ability, it is impaired to have avoided the collision to make unmanned aerial vehicle body 1 inside and outside spare part, thereby promote unmanned aerial vehicle body 1's life, unmanned aerial vehicle body 1's lower surface is provided with support frame 9, it is more steady when making unmanned aerial vehicle body 1 descend through setting up of support frame 9.
Further, side protector 4 includes first side lever 401, first spring 402, second side lever 403 and arc 404, and the inside of first side lever 401 is provided with first spring 402, and the one end fixedly connected with second side lever 403 of first spring 402, the top fixedly connected with arc 404 of second side lever 403, through the side of first spring 402 and arc 404 setting up to unmanned aerial vehicle body 1 provide the buffering protection and prevent that blade 11 is impaired.
Further, top protector 7 includes first mounting panel 701, bracing piece 702, second spring 703 and roof 704, and the last fixed surface of first mounting panel 701 is connected with bracing piece 702, and the inside of first bracing piece 702 is provided with second spring 703, and the top fixedly connected with roof 704 of second spring 703 can cushion the protection for the upper surface of unmanned aerial vehicle body 1 through the setting of roof 704 and second spring 703.
Further, front protector 8 includes second mounting panel 801, connecting rod 802, third spring 803 and baffle 804, and one side fixedly connected with connecting rod 802 of second mounting panel 801, the inside of connecting rod 802 are provided with third spring 803, and the one end fixedly connected with baffle 804 of third spring 803 can cushion for the front of unmanned aerial vehicle body 1 through the setting of baffle 804 and third spring 803 and protect.
Further, support frame 9 includes support body 901 and sucking disc 902, and the lower surface of support body 901 is provided with sucking disc 902, and it is more steady when making unmanned aerial vehicle body 1 descend to increase the land fertility through setting up of sucking disc 902.
Further, the upper surface of connecting block 2 is provided with rotary mechanism 10, and rotary mechanism 10's upper end is provided with blade 11, makes unmanned aerial vehicle body 1 can take off and descend through rotary mechanism 10 and blade 11's setting.
The working principle is as follows: install protector earlier, screw hole 5 that the inside of connecting block 2 and connector 3 was seted up earlier during the installation aligns, insert screw hole 5 with bolt 6 again and screw up and can accomplish the installation, the structure is convenient for install and dismantle, it is more convenient to change when protector damages, when unmanned aerial vehicle body 1 receives the collision at the flight process, side protector 4, top protector 7 and front protector 8 can provide a buffer protection's effect to each face of unmanned aerial vehicle body 1, very big promotion unmanned aerial vehicle body 1's anticollision ability, it is impaired to have avoided the collision to make unmanned aerial vehicle body 1 inside and outside spare part, thereby promote unmanned aerial vehicle body 1's life, when support body 901 and sucking disc 902 make unmanned aerial vehicle body 1 descend, it is more steady when increasing the land fertility of grabbing makes unmanned aerial vehicle body 1 descend.
It will be evident to those skilled in the art that the utility model is not limited to the details of the foregoing illustrative embodiments, and that the present invention may be embodied in other specific forms without departing from the spirit or essential attributes thereof. The present embodiments are therefore to be considered in all respects as illustrative and not restrictive, the scope of the utility model being indicated by the appended claims rather than by the foregoing description, and all changes which come within the meaning and range of equivalency of the claims are therefore intended to be embraced therein. Any reference sign in a claim should not be construed as limiting the claim concerned.
Claims (6)
1. The utility model provides an unmanned aerial vehicle flight buffer stop, includes unmanned aerial vehicle body (1) and connecting block (2), its characterized in that: the utility model discloses an unmanned aerial vehicle, including unmanned aerial vehicle body (1), one end fixedly connected with connector (3) of connecting block (2), one side fixedly connected with side protector (4) of connector (3), threaded hole (5) are all seted up to the inside of connecting block (2) and connector (3), the internal thread of threaded hole (5) is connected with construction bolt (6), the last fixed surface of unmanned aerial vehicle body (1) is connected with top protector (7), the positive fixedly connected with front protector (8) of unmanned aerial vehicle body (1), the lower surface of unmanned aerial vehicle body (1) is provided with support frame (9).
2. The unmanned aerial vehicle flight buffer stop of claim 1, characterized in that: the side protection device (4) comprises a first side rod (401), a first spring (402), a second side rod (403) and an arc-shaped plate (404), wherein the first spring (402) is arranged inside the first side rod (401), the second side rod (403) is fixedly connected to one end of the first spring (402), and the arc-shaped plate (404) is fixedly connected to the top end of the second side rod (403).
3. The unmanned aerial vehicle flight buffer stop of claim 1, characterized in that: the top protection device (7) comprises a first mounting plate (701), a supporting rod (702), a second spring (703) and a top plate (704), wherein the supporting rod (702) is fixedly connected to the upper surface of the first mounting plate (701), the second spring (703) is arranged inside the supporting rod (702), and the top end of the second spring (703) is fixedly connected with the top plate (704).
4. The unmanned aerial vehicle flight buffer stop of claim 1, characterized in that: the front protection device (8) comprises a second mounting plate (801), a connecting rod (802), a third spring (803) and a baffle (804), wherein the connecting rod (802) is fixedly connected to one side of the second mounting plate (801), the third spring (803) is arranged inside the connecting rod (802), and the baffle (804) is fixedly connected to one end of the third spring (803).
5. The unmanned aerial vehicle flight buffer stop of claim 1, characterized in that: the support frame (9) comprises a frame body (901) and a sucker (902), wherein the sucker (902) is arranged on the lower surface of the frame body (901).
6. The unmanned aerial vehicle flight buffer stop of claim 1, characterized in that: the upper surface of connecting block (2) is provided with rotary mechanism (10), rotary mechanism's (10) upper end is provided with blade (11).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202121782847.1U CN215514154U (en) | 2021-08-02 | 2021-08-02 | Unmanned aerial vehicle flight buffer stop |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202121782847.1U CN215514154U (en) | 2021-08-02 | 2021-08-02 | Unmanned aerial vehicle flight buffer stop |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN215514154U true CN215514154U (en) | 2022-01-14 |
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ID=79788834
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202121782847.1U Active CN215514154U (en) | 2021-08-02 | 2021-08-02 | Unmanned aerial vehicle flight buffer stop |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN215514154U (en) |
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2021
- 2021-08-02 CN CN202121782847.1U patent/CN215514154U/en active Active
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